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1. 发明授权

US3546996A Release latch actuated by temperature excursion 失效
标题翻译：释放由温度驱动器执行的锁定
公开(公告)号：US3546996A
公开(公告)日：1970-12-15
申请号：US3546996D
申请日：1969-04-10
申请人： ATOMIC ENERGY COMMISSION
发明人： GRIJALVA RAMON J , QUEENER GEORGE F
IPC分类号： A62C35/60 , F16B31/00
CPC分类号： A62C35/605 , F16B31/007

2. 发明授权

US12071970B2 Thermally stabilized fastener system and method 有权
公开(公告)号：US12071970B2
公开(公告)日：2024-08-27
申请号：US17981407
申请日：2022-11-05
申请人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
发明人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
IPC分类号： F16B31/04 , C22F1/18 , F16B31/00 , F16B31/06 , F16B43/00
CPC分类号： F16B31/04 , C22F1/183 , F16B31/007 , F16B31/06 , F16B43/001
摘要： A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

3. 发明申请

US20070158127A1 On-vehicle component fixation-release apparatus 失效
标题翻译：车载部件固定释放装置
公开(公告)号：US20070158127A1
公开(公告)日：2007-07-12
申请号：US10591154
申请日：2005-03-03
申请人： Katsuaki Taguchi , Yuta Urushiyama , Suguru Yoshida
发明人： Katsuaki Taguchi , Yuta Urushiyama , Suguru Yoshida
IPC分类号： B60K28/00
CPC分类号： B60R22/321 , B60N2/015 , B60R21/017 , B60R2021/01252 , E05D5/0207 , E05D7/121 , E05Y2800/684 , E05Y2900/538 , F16B1/0014 , F16B31/007 , F16B2001/0078
摘要： To readily remove on-vehicle components from a vehicle body, suitably reflecting the state of the vehicle or occupant in addition to the will of the operator. The safety confirmation device 11 determines whether or not to permit actuation of the separation actuator 13, that is, whether to set the switch 12 to the ON state to allow an electrical connection from the power supply 14 to the separation actuator 13, based on the signals input from the external input receiving portion 21, the occupant protection device 22, the status quantity sensor 23, and the input portion 24, and outputs a gate signal corresponding to this determination result to the switch 12. Electrification of the separation actuator 13 from the power supply 14 via the switch 12 releases the fixation of an on-vehicle component by disassembling the fixation member that fixes the on-vehicle component to the vehicle body.
摘要翻译：为了容易地从车体移除车载部件，除了操作者的意愿之外，适当地反映车辆或乘员的状态。安全确认装置11基于是否允许分离致动器13的致动，即是否将开关12设定为接通状态来确定是否允许从电源14到分离致动器13的电连接从外部输入接收部分21，乘员保护装置22，状态量传感器23和输入部分24输入的信号，并将与该确定结果相对应的门信号输出到开关12。分离致动器13经由开关12从电源14通电，通过拆卸将车载部件固定到车体的固定部件来释放车载部件的固定。

4. 发明授权

US12071969B2 Thermally stabilized fastener system and method 有权
公开(公告)号：US12071969B2
公开(公告)日：2024-08-27
申请号：US17981406
申请日：2022-11-05
申请人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
发明人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
IPC分类号： F16B31/04 , C22F1/18 , F16B31/00 , F16B31/06 , F16B43/00 , C21D7/00
CPC分类号： F16B31/04 , C22F1/183 , F16B31/007 , F16B31/06 , F16B43/001 , C21D7/00
摘要： A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

5. 发明申请

US20170327251A1 Passive Device Designed to Facilitate Demise of A Space System During Re-Entry Into the Earth's Atmosphere 审中-公开
公开(公告)号：US20170327251A1
公开(公告)日：2017-11-16
申请号：US15532346
申请日：2015-12-01
申请人： Thales Alenia Space Italia S.p.A. Con Unico Socio
发明人： Guido Parissenti , Primo Attina' , Roberto Destefanis , Corrado Gennaro , Lilith Grassi , Marco Nebiolo
IPC分类号： B64G1/62 , B64G1/64 , B64G1/10 , F16B31/00
CPC分类号： B64G1/62 , B64G1/10 , B64G1/1021 , B64G1/64 , B64G1/641 , B64G2001/1092 , F16B31/007
摘要： Space system comprising a structure formed by structure components, an on-board equipment carried by the structure, and a passive device designed to facilitate demise of the space system during re-entry into the Earth's atmosphere. The passive device comprises connecting members designed to stably connect the structure components. The connecting members comprise at least a portion made of a primer material with characteristics such as to decay at re-entry altitudes higher than those at which the current connecting members melt so as to make unstable the connection created by the connecting members to such an extent as to early triggering demise of the structure of the space system during re-entry into the Earth's atmosphere.

6. 发明授权

US5695306A Fusible member connection apparatus and method 失效
标题翻译：易熔件连接装置及方法
公开(公告)号：US5695306A
公开(公告)日：1997-12-09
申请号：US646588
申请日：1996-05-08
申请人： William D. Nygren, Jr.
发明人： William D. Nygren, Jr.
IPC分类号： B64G1/64 , F15B15/19 , F15B15/26 , F16B31/00 , F16B37/08 , F16B39/36
CPC分类号： F15B15/261 , B64G1/641 , B64G1/645 , F15B15/19 , F16B31/007 , Y10T29/49821
摘要： A connection apparatus utilizes a structural element made of fusible material supported directly in the connection load path of the device. A carrier mechanism is axially translatably supported in the device and utilizes a connecting member to connect two desired structures. The connection mechanism engages and holds the connecting member in a first axial position. In one embodiment, the connection mechanism releases the connecting member when translated to a second axial position. In another embodiment the connection mechanism tensions the connection when translated to the a second axial position. The fusible member is heated to transition from solid to liquid. In the liquid state, the fusible member no longer opposed axial load on the carrier mechanism. The fusible alloy comprises a low melting temperature alloy, such as bismuth-lead or bismuth-tin.
摘要翻译：连接装置利用由直接支撑在装置的连接负载路径中的可熔材料制成的结构元件。承载机构被轴向平移地支撑在装置中并且利用连接构件来连接两个期望的结构。连接机构将连接构件接合并保持在第一轴向位置。在一个实施例中，当平移到第二轴向位置时，连接机构释放连接构件。在另一个实施例中，当平移到第二轴向位置时，连接机构使连接件拉紧。可熔体被加热以从固体转变成液体。在液体状态下，可熔构件不再反对载体机构上的轴向载荷。熔融合金包括低熔点合金，例如铋铅或铋锡。

7. 发明申请

WO2010031377A2 FLUGKÖRPER MIT ZUMINDEST EINEM BREMSFALLSCHIRM SOWIE BEFESTIGUNGSVORRICHTUNG ZUR BEFESTIGUNG EINES BREMSFALLSCHIRMS AN EINEM FLUGKÖRPER 审中-公开
标题翻译：与至少一个制动伞的导弹和固定装置，用于固定漏斗形减速伞IN A导弹
公开(公告)号：WO2010031377A2
公开(公告)日：2010-03-25
申请号：PCT/DE2009/001240
申请日：2009-09-03
申请人： LFK-LENKFLUGKÖRPERSYSTEME GMBH , FASOL, Dieter , GRABMEIER, Michael
发明人： FASOL, Dieter , GRABMEIER, Michael
IPC分类号： B64D17/80 , B64D17/38 , F42B10/56 , F16B31/00
CPC分类号： F42B10/56 , F16B31/007
摘要： Ein Flugkörper mit zumindest einem Bremsfallschirm (2), wobei der Flugkörper (1;1 ') mit zumindest einer Befestigungsvorrichtung (3; 3', 3") für den Bremsfallschirm (2) versehen ist und wobei zwischen der Befestigungsvorrichtung (3; 3', 3") und dem Bremsfallschirm (2) eine Zugleine (4) vorgesehen ist, zeichnet sich dadurch aus, dass die Befestigungsvorrichtung (3; 3', 3") derart am Flugkörper (1; 1') angebracht ist, dass eine im entfalteten Zustand des von Luft angeströmten Bremsfallschirms (2) von der Zugleine (4) gebildete gerade Linie in ihrer gedachten Verlängerung (G) durch den Schwerpunkt (S) des Flugkörpers (1; 11) verläuft.
摘要翻译：具有至少一个漏斗形减速伞（2），其中，所述导弹（1; 1“）一种导弹与至少一个紧固装置（3; 3”，3“），用于制动降落伞（2）的固定装置（3之间，并且其中; 3' ，3“）和制动降落伞（2）一个拉绳（4）设置，其特征在于，所述固定装置（3; 3”，3" ，在这样的方式）上的导弹（1; 1' ）被安装在通过导弹的比重（S）的中心在它的假想延长（G）的线（4）刚刚形成的线的空气制动降落伞（2）的入射流量的展开状态（1; 11）。

8. 发明申请

WO2010031377A3 FLYING OBJECT COMPRISING AT LEAST ONE BRAKE PARACHUTE AND FIXING DEVICE FOR FIXING A BRAKE PARACHUTE TO A FLYING OBJECT 审中-公开
标题翻译：与至少一个制动伞的导弹和固定装置，用于固定漏斗形减速伞IN A导弹
公开(公告)号：WO2010031377A3
公开(公告)日：2010-06-10
申请号：PCT/DE2009001240
申请日：2009-09-03
申请人： LFK GMBH , FASOL DIETER , GRABMEIER MICHAEL
发明人： FASOL DIETER , GRABMEIER MICHAEL
IPC分类号： B64D17/80 , B64D17/38 , F16B31/00 , F42B10/56
CPC分类号： F42B10/56 , F16B31/007
摘要： The invention relates to a flying object comprising at least one brake parachute (2), said flying object (1; 1') being provided with at least one fixing device (3; 3', 3") for the brake parachute (2) and with a drag line (4) between the fixing device (3; 31, 3") and the brake parachute (2). The object is characterised in that the fixing device (3; 3', 3") is attached to the flying object (1; 1') in such a way that when the brake parachute (2) is open and filled with air, the imaginary extension (G) of the straight line formed by the drag line (4) runs through the centre of gravity (S) of said flying object (1; 11).
摘要翻译：具有至少一个漏斗形减速伞（2），其中，所述导弹（1; 1“）一种导弹与至少一个紧固装置（3; 3”，3“），用于制动降落伞（2）的固定装置（3之间，并且其中; 3' ，3“）和制动降落伞（2）一个拉绳（4）设置，其特征在于，所述固定装置（3; 3”，3" ，在这样的方式）上的导弹（1; 1' ）被安装在通过导弹的比重（S）的中心在它的假想延长（G）的线（4）刚刚形成的线的空气制动降落伞（2）的入射流量的展开状态（1; 11）。

9. 发明授权

US11867217B2 Thermally stabilized fastener system and method 有权
公开(公告)号：US11867217B2
公开(公告)日：2024-01-09
申请号：US17981401
申请日：2022-11-05
申请人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
发明人： James Alan Monroe , Jeremy Sean McAllister , Jay Russell Zgarba
IPC分类号： F16B31/04 , F16B43/00 , F16B31/00 , F16B31/06 , C22F1/18
CPC分类号： F16B31/04 , C22F1/183 , F16B31/007 , F16B31/06 , F16B43/001
摘要： A thermally stabilized fastener system and method is disclosed. The disclosed system/method integrates a fastener (FAS) incorporating a faster retention head (FRH), fastener retention body (FRB), and fastener retention tip (FRT) to couple a mechanical member stack (MMS) in a thermally stabilized fashion using a fastener retention receiver (FRR). The MMS includes a temperature compensating member (TCM), a first retention member (FRM), and an optional second retention member (SRM). The TCM is constructed using a tailored thermal expansion coefficient (TTC) that permits the TCM to compensate for the thermal expansion characteristics of the FAS, FRM, and SRM such that the force applied by the FRH and FRR portions of the FAS to the MMS is tailored to a specific temperature force profile (TFP) over changes in MMS/FAS temperature. The TCM may be selected with a TTC to achieve a uniform TFP over changes in MMS/FAS temperature.

10. 发明申请

US20170284443A1 THERMALLY FRAGMENTABLE FASTENING DEVICE 审中-公开
公开(公告)号：US20170284443A1
公开(公告)日：2017-10-05
申请号：US15473289
申请日：2017-03-29
申请人： Airbus DS GmbH
发明人： Mathias Von Alberti
IPC分类号： F16B31/00 , B64G1/64 , B64G1/62
CPC分类号： F16B31/007 , B64G1/62 , B64G1/64 , B64G1/645 , F16B31/00
摘要： A fastening device for use in a spacecraft comprises a shaft and a head, which is connected by a first solder to the shaft. The first solder comprises a material of which the melting point is lower than the temperature acting on the fastening device on re-entry of a spacecraft equipped with fastening device into the earth's atmosphere.

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